DO-297 Training | IMA Development Guidance
DO-297 training covers the concepts, methods, and requirements to develop and maintain a successful DO-297 standard. DO-297 training course provides the foundation for creating Integrated Modular Avionics (IMA) system and its correlation to RTCA/DO-297 guidance and certification considerations.
Integrated Modular Avionics (IMA) Definition
Integrated Modular Avionics is referred to a communal series of adaptable, reusable, and interoperable resources of hardware and software that develops a platform that delivers services, planned and verified to a distinct series of safety and execution requirements, operations associated with host applications execution aircraft.
- IMA is an inattentive method to HW/SW, SW/SW, and HW/HW interfaces.
- IMA is a retreat from federations of devoted or specialty processors
- Differences between the federated systems and IMA systems are particular and provided systems may integrate components of both.
IMA Characteristics
- Mutual resources
- Platform self-governing application process
- Movable applications
- Expandable/reconfigurable with narrow influences
- Increased configuration management complications
Added Value of DO-297 IMA Guideline Training
- Integrated Modular Avionics
- IMA and DO-297 strengths and weaknesses
- Evolutionary path of IMA and DO-297
- Verification and validation
- Common mistakes and how to avoid them
- Certification bases
- DO-297 and ARP-4754A
- Safety evaluation
- Development assurance levels
- Configuration management
- Certification liaison
- DO-297 application approval
Audience
DO-297 training is a 2-day course designed for:
- Developers of IMA systems
- Integrators of IMA systems
- Managers and supervisors
- Project managers
- All professionals who are involved in developing IMA DO-297 guidelines
What Will You Learn?
Below are the major topics this training will cover. For more details click HERE.
- Overview of DO-297
- Fundamentals of Avionics Embedded Systems
- DO-297 Certification Steps
- Regulations, Standards, and Guidance
- AC 20-170 and TSO C-153
- IMA System Characteristics
- Federated vs IMA Architecture
- IMA Features
- Differences between ARINC 653 and DO-297
- Partitioned Avionic Software
- Examples of Aircrafts Using IMA
- TONEX Case Study Sample: NASA IV&V Mission
DO-297 Training | IMA Development Guidance